Control System Design of Missile Based on Back-Stepping and Variable Structure Control Method

Yuan Gao; Yong Xia; Xu Wang; Wu Zhang

doi:10.4028/www.scientific.net/AMM.644-650.516

Paper Titles

Panoramic Vision System for Autonomous Driving Vehicle
p.497

Improved Method of High Voltage Switchgear Temperature Prediction Based on WNN
p.502

Geometry Error Parameters Identification Methods of 3-Coordinate CNC Machine Tools
p.506

A Multi-Axis Synchronization Control Approach Based on Adjacent Cross-Coupling Strategy
p.510

Control System Design of Missile Based on Back-Stepping and Variable Structure Control Method
p.516

Speed Synchronization System of Master-Slave Motor Based on Repetitive Control
p.523

Hydrodynamical Analysis on the Arrow
p.527

Study on the Mechanism of Resonance Inducing V-Shaped Notch Tip Crack
p.531

Description of Subway DT Series Fastening
p.535

HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 644-650Control System Design of Missile Based on...

Control System Design of Missile Based on Back-Stepping and Variable Structure Control Method

Abstract:

A nonlinear decoupling control method based on back-stepping design and sliding variable structure control theory was proposed in this paper according to the nonlinear and strong coupling characteristics of missile at hingh angle of attack. The affine nonlinear model of missile was firstly established, the exact linearization and input/output decoupling of system were then realized using differential geometry theory. On the basis of this, the robust controller was designed using back-stepping design and variable structure control method. Simulation results indicate that the influences caused by missile parameter uncertainties, unsuited uncertainties with known upper boundaries and stochastic interference can be effectively restrained.

You might also be interested in these eBooks

View Preview

Info:

Periodical:

Applied Mechanics and Materials (Volumes 644-650)

Pages:

516-522

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.644-650.516

Citation:

Cite this paper

Online since:

September 2014

Authors:

Yuan Gao*, Yong Xia, Xu Wang, Wu Zhang

Keywords:

Back-Stepping Design, Differential Geometry, Variable Structure Control

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

* - Corresponding Author

References

[1] Hu Yueming. Nonlinear Control Theory and Application. Beijing: National Defense Press. (2002).

Google Scholar

[2] Cao Jianfu, Han Congzhao, Fang Yangwang. Nonlinear System Theory and Application. Xi'an: Xi'an Jiao Tong University Press, (2006).

Google Scholar

[3] Kim K. S. and Kim Y. Backstepping Control of Rigid Spacecraft Slew Maneuver. AIAA 2001-4210, (2001).

DOI: 10.2514/6.2001-4210

Google Scholar

[4] Sharma M., Farrell J. A. and Polycarpou M. Backstepping Flight Control Using On-Line Function Approximation. AIAA 2003-5713, (2003).

DOI: 10.2514/6.2003-5713

Google Scholar

[5] Slotine J. J. and Sastry S. S. Tracking Control of Nonlinear Systems Using Sliding Surfaces with Application to Robot Manipulators. Int. J. Control, 1983, 38(2): 465-492.

DOI: 10.1080/00207178308933088

Google Scholar

[6] Esfandlary F. and Khalil H. K. Stability Analysis of A Continuous Implementation of Variable Structure Control. IEEE Trans. Automatic Control, 1991, 36(5): 616-619.

DOI: 10.1109/9.76367

Google Scholar